TY - GEN
T1 - Robust gain scheduled control of a space launcher by introducing LQG/LTR ideas in the NCF robust stabilisation problem
AU - Abbas-Turki, Mohamed
AU - Duc, Gilles
AU - Clement, Benoît
AU - Theodoulis, Spilios
PY - 2007/12
Y1 - 2007/12
N2 - A space launcher is a time-varying plant which is known to be hard to control, due to time and frequency-domain constraints and parameters uncertainties. In this paper, this problem is solved by interpolating LTI controllers designed for different instants of the flight. Such controllers are obtained by combining the NCF robust control problem with the LQG/LTR approach, the later being useful to design the compensators included in the first one.
AB - A space launcher is a time-varying plant which is known to be hard to control, due to time and frequency-domain constraints and parameters uncertainties. In this paper, this problem is solved by interpolating LTI controllers designed for different instants of the flight. Such controllers are obtained by combining the NCF robust control problem with the LQG/LTR approach, the later being useful to design the compensators included in the first one.
UR - http://www.scopus.com/inward/record.url?scp=62749169243&partnerID=8YFLogxK
U2 - 10.1109/CDC.2007.4434356
DO - 10.1109/CDC.2007.4434356
M3 - Conference contribution
AN - SCOPUS:62749169243
SN - 1424414989
SN - 9781424414987
T3 - Proceedings of the IEEE Conference on Decision and Control
SP - 2393
EP - 2398
BT - Proceedings of the 46th IEEE Conference on Decision and Control 2007, CDC
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 46th IEEE Conference on Decision and Control 2007, CDC
Y2 - 12 December 2007 through 14 December 2007
ER -